Investigations on a STOL-airplane with internally blown flaps are described. To avoid flow separation on the wing, slots were located behind the nose flap and in front of the trailing edge flap. Maximum lift and optimum L/D were investigated, as well as the effectiveness of the aileron and the horizontal tail. (Author)


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    Title :

    Three Component Measurements on a Light STOL Aircraft with Chordwise Blowing


    Contributors:
    H. Koerner (author) / R. Loehr (author)

    Publication date :

    1975


    Size :

    23 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English








    STOL AIRCRAFT

    MOMBRINIE BRUNO | European Patent Office | 2020

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